pdf

PID Adjustment Principle and Multi-axis Aircraft Setting Guide

  • 2020-11-30
  • 123.31KB
  • Points it Requires : 1

PID: Billy-Integral-Differential When the multi-rotor aircraft has any angle change on the PITCH/ROLL/YAW axis, the gyroscope will output the deviation angle value relative to the initial position. The flight control uses the \"PID\" program algorithm to drive the motor based on the recorded original position to return the multi-rotor aircraft to the initial position. This is a combination of data sampling over time and predicting future positions based on the measured angle deviation. The information it provides is enough for the flight control to drive the motor to return the multi-rotor aircraft to a balanced state. The P value is the most important part of the PID, which directly determines the flight effect of the aircraft.

unfold

You Might Like

Uploader
太白金星
 

Recommended ContentMore

Popular Components

Just Take a LookMore

EEWorld
subscription
account

EEWorld
service
account

Automotive
development
circle

About Us Customer Service Contact Information Datasheet Sitemap LatestNews


Room 1530, 15th Floor, Building B, No.18 Zhongguancun Street, Haidian District, Beijing, Postal Code: 100190 China Telephone: 008610 8235 0740

Copyright © 2005-2024 EEWORLD.com.cn, Inc. All rights reserved 京ICP证060456号 京ICP备10001474号-1 电信业务审批[2006]字第258号函 京公网安备 11010802033920号
×